Compositions and Methods for Treating Nuclear Fuel

ABSTRACT

Compositions are provided that include nuclear fuel. Methods for treating nuclear fuel are provided which can include exposing the fuel to a carbonate-peroxide solution. Methods can also include exposing the fuel to an ammonium solution. Methods for acquiring molybdenum from a uranium comprising material are provided.

STATEMENT OF GOVERNMENT SUPPORT

This invention was made with Government support under Contract DE-AC05-76RLO1830 awarded by the U.S. Department of Energy. The Government has certain rights in the invention.

TECHNICAL FIELD

The present disclosure relates generally to compositions and the treatment of uranium-comprising materials. Particular embodiments of the disclosure relate to compositions and methods as well as systems for treating nuclear fuel.

BACKGROUND

As part of the process for utilizing nuclear fuel to generate power, the fuel is irradiated. The fuel can be, for example, UO₂-based fuel, Mixed Oxide (MOX) fuels, and/or U-metal fuels. Irradiated nuclear fuel can be the product of the irradiation of many kinds of commercial fuels as well as defense fuels, and these fuels can be classified as spent fuel and/or irradiated uranium.

Processing this fuel, either before or after irradiation, can be problematic. Irradiated fuel can be particularly problematic in view of the various transmutated and fission products that are generated. Problems associated with the processing can include environmental and/or health hazards as well as problems associated with nuclear material safeguards and security, cost, storage, and/or disposal.

From an environmental and/or health standpoint for example, the fuel can contain components that have been classified as environmentally hazardous and/or toxic that must meet regulatory processing and disposition requirements. For example, certain actinide and fission products can dictate handling fuel according to comparably expensive methods rather than comparably inexpensive methods were such components below regulated levels. This handling can include highly regulated storage and/or disposal techniques. Also, previous processing techniques can introduce and/or generate environmentally hazardous components such as organic solvents and/or NO_(X), for example.

Further, the fuel contains valuable components whereby the recycling or extraction of such components is highly desirable. Uranium and/or plutonium within the fuel, for example, are valuable components that if recycled can provide for more cost efficient fuel and energy production as well as less waste for storage and/or disposal. In addition, the extraction of industrial- and medically-useful radioisotopes such as molybdenum-99 can be desirable.

In the past, these fuels have been treated according to what is referred to as the Plutonium and Uranium Extraction (PUREX) process. Generally, the fuel has been exposed to a hot nitric acid bath to isolate the uranium by oxidizing the UO₂ to UO₂ ²⁺, for example. This process can dissolve the fuel matrix as well as all the fission products. While a great deal of energy is necessary to dissolve the fuel in hot nitric acid, aside from this additional energy expense, as the UO₂ fuel is dissolved in the nitric acid, a large volume of NO and NO₂ gases are formed and sent up processing stacks. Some noble gas fission products such as xenon and krypton can be completely released and proceed up the stacks as well. It has been found that fission products such as iodine and bromine also appear in the stack gases. Ruthenium also evaporates and can condense in the stacks. Tritium can be expelled up the stacks as well. Undissolved components of the hot nitric acid treatment can remain, and these components can include Mo, Tc, Ru, Rh, and Pd.

Following the nitric acid extraction, organic extractants such as tributyl phosphate (TBP) are dissolved in organic solvents and used to facilitate the separation of the actinides from each other and from other fission products. Problematically, these processing techniques accumulate combustible organic solvents and corrosive acids which can result in radiation induced solvent degradation. Further, valuable actinides may be lost among fission product waste and highly radiotoxic mixed wastes may be generated.

SUMMARY

Compositions are provided that include irradiated nuclear fuel and ammonium. According to example implementations, the compositions can include the irradiated nuclear fuel and alkaline carbonates such as ammonium carbonate. Compositions are also provided that include irradiated nuclear fuel; carbonate; and peroxide.

Methods for treating irradiated nuclear fuel are provided. The methods can include exposing the fuel to a carbonate-peroxide solution to dissolve at least a portion of the uranium into the solution. Methods can also include exposing the fuel to an ammonium solution to dissolve at least a portion of the uranium into the solution, and removing at least some of the ammonium from the solution to acquire the uranium. Methods can include preparing a mixture comprising the fuel and an aqueous solution; and maintaining the mixture below a temperature of about 100° C. while dissolving at least a portion of the uranium of the fuel into the solution.

Methods for acquiring molybdenum from a uranium comprising material are provided. The methods can include exposing the material to an aqueous solution to form a mixture comprising a solid phase and a liquid phase; separating the solid phase from the liquid phase; and exposing at least a portion of the liquid phase to an adsorbent to remove at least some of the solute from the liquid phase and form an effluent containing the molybdenum.

DRAWINGS

Embodiments of the disclosure are described below with reference to the following accompanying drawings.

FIG. 1 is a system for treating irradiated nuclear fuel according to an embodiment.

FIG. 2 is a process scheme according to an embodiment.

FIG. 3 is a process scheme according to an embodiment.

FIGS. 4A and 4B are a process scheme according to an embodiment.

FIG. 5 is a process scheme according to an embodiment.

FIGS. 6A and 6B are another process scheme according to an embodiment.

DESCRIPTION

This disclosure is submitted in furtherance of the constitutional purposes of the U.S. Patent Laws “to promote the progress of science and useful arts” (Article 1, Section 8).

The compositions, methods and systems of the present disclosure will be described with reference to FIGS. 1-6B. Referring first to FIG. 1, a general depiction of a system is shown that may be utilized to provide the compositions and/or perform the methods as described herein. As depicted, system 10 can be considered a continuous dissolution system; however, other systems may be utilized. For example, systems configured to perform processes such as decanting and/or batch filtration may be utilized. System 10 can include a vessel 14 and material 16. Vessel 14 can be coupled to conduit 12 as well as conduit 18. Vessel 14 may be configured to also include a filter material 20. Filter material 20 can be configured to support material 16 and act to confine solid material within vessel 14 while allowing liquid materials to pass through to conduit 18.

According to example implementations, the volume confined by vessel 14 can be in fluid communication with both conduits 12 and 18. Conduits 12 and 18 can be coupled with pumps and/or valves to facilitate the metered transfer of a solution through vessel 14. System 10 may be utilized to expose the solution to material 16. According to example implementations, this metered transfer can facilitate the dissolution of material 16 using the solution provided from conduit 12.

Material 16 can be irradiated nuclear fuel such as the irradiated nuclear fuel noted above. This fuel can include uranium, transuranics such as plutonium, and/or fission products. It is understood that the chemistry of irradiated nuclear fuel is complex as well as unpredictable, making the treatment of irradiated nuclear fuel difficult and not simply a matter of routine experimentation. The composition of the irradiated nuclear fuel can vary widely depending on the original fuel composition and the type of irradiation performed. The nuclear fuel may have been manufactured for industrial or defense purposes and may have been irradiated according to either protocol. These variables can change the chemistry of the fuel dramatically. To further complicate matters, the irradiated fuel may have been treated after irradiation. For example, material 16 can be oxidized prior to processing as described herein and as oxidized, material 16 may include U₃O₈ and/or UO₃, for example.

Material 16 can be in the form of pellets, for example, maintaining the shape in which it was manufactured for irradiation. According to example implementations, material 16 can be comprised of particles having average sizes of less than 200 μm. According to other example implementations, the particles can have an average size from about 5 to about 200 μm. The size can also range from about 25 μm to about 200 μm, and in other implementations, the size can range from about 5 μm to about 25 μm.

System 10 can be configured to expose a solution to material 16 within vessel 14. The solution can include one or more of carbonate, peroxide, and ammonium, such as an ammonium cation. The solution can be a carbonate-peroxide solution, an ammonium solution, and/or an ammonium carbonate solution. According to an example implementation, the solution can include ammonium carbonate and peroxide. While ammonium carbonate can be utilized, other carbonates such as sodium carbonate and potassium carbonate may be utilized as well. Ammonium carbonate may be preferred because it can be removed from the product solution via evaporation.

The peroxide can be in the form of hydrogen peroxide. The peroxide within the solution may be at least 0.05 M, for example. The solution may contain at least 0.1 M carbonate species, which may be in the form of ammonium carbonate, for example. The ammonium carbonate within the solution may be at least 0.1 M of the solution prior to being exposed to the material 16. The solution may also be saturated with carbonate species or as high as 2.2 M in some instances. According to example implementations, the ammonium carbonate within the solution can be greater than the concentration of peroxide within the solution. The solution can be saturated with ammonium carbonate and also include 30% (v/v) of a 30% (wt/wt) hydrogen peroxide solution. The solution may have pH>7 and may be as high as 10 or higher. The solution can be exposed to material 16 at room temperature and atmospheric pressure, for example.

Upon being exposed to material 16, the solution and material 16 can form a composition such as a mixture. The mixture can be heterogeneous and include both a solid and liquid phase. According to example implementations, the mixture within vessel 14 can include the irradiated fuel as well as ammonium. The mixture within vessel 14 can include the irradiated nuclear fuel as well as carbonate and peroxide. The mixture can also have at least some of the ammonium comprised of the liquid phase, and at least some of the solid phase comprising the fission products. As disclosed, at least some of the uranium of material 16 within vessel 14 can then be comprised of the liquid phase upon dissolution of material 16 with the solution.

According to example implementations, upon exposure of material 16 to the solution, the uranium within material 16 may oxidize and form a series of carbonate-peroxide complexes. These complexes may ultimately convert to the soluble UO₂(CO₃)₃ ⁴⁻, becoming part of the liquid phase The mixture can also include fission products and transuranics which can precipitate as carbonates and hydroxides, thus remaining in the solid phase. The noble metal phase of the irradiated fuel may form a black suspension in the product, thereby remaining in the solid phase as well. According to example embodiments, the partitioning of components of material 16 is detailed in the remaining Figures.

Referring to FIG. 2, a general scheme for the processing of material 16 is shown wherein material 16 is exposed to the solution containing carbonate and peroxide to form a liquid phase, a solid phase, and a gas phase, for example. Upon exposure of material 16 to the solution, the UO₂ can oxidize and dissolve, forming a series of soluble peroxide carbonate complexes which enter the liquid phase. The peroxide within the solution can decompose within a few hours, leaving the dissolved uranium in the uranium oxide carbonate form described. The ammonium salt of this anion may be only moderately soluble and strong ammonium carbonate solutions may precipitate large yellow crystals of (NH₄)₄UO₂(CO₃)₃ (ammonium uranyl carbonate). This compound may be redissolved by reducing the ammonium carbonate concentration to about 0.05 M, thus returning the complex to the liquid phase.

Additional hydrogen peroxide may also be utilized to dissolve the ammonium uranyl carbonate into the liquid phase. Several fission products and transuranic elements can form moderately soluble carbonate complexes and be a part of the M-CO₃(/) shown in FIG. 2 at high carbonate concentration. The lanthanides, zirconium, and Pu(IV) may be a part of these carbonates. Where the carbonate concentration is reduced, perhaps later in the process through the evaporation of the ammonium carbonate complex, these moderately soluble carbonate complexes may precipitate and return to the solid phase.

The M-CO₃(/) of the liquid phase can include UO₂(CO₃)₃ ⁴⁻ and dilute (NH₄)₂CO₃ with various fission products. The liquid phase can have substantially all of the Cs⁺ and Rb⁺ and part of the Mo and Tc (as MoO₄ ²⁻ and TcO₄ ⁻). The liquid phase can also contain Se and Te (as, for example, SeO₃ ²⁻ and TeO₃ ²⁻) as well as most of the Br and I (as Br⁻ and I⁻). The liquid phase can also contain Pd as cationic ammine complexes. Lanthanides, actinides, and Zr can be present at a low concentration as carbonate complexes.

As shown in FIG. 2, there is an off gas (OG) or gas phase that may be generated during the process. This OG phase can include O₂ via the decomposition of peroxide. Other gases that may evolve can include NH₃, CO₂, and H₂O. Small amounts of Xe and Kr may also appear in the OG phase. According to example implementations, the noble gas fission products may be captured from this process. The Xe and Kr can be absorbed onto a silica gel at −20° C. after freezing the water and ammonium carbonate on a cold finger cooled with dry ice, for example while allowing oxygen to pass into the atmosphere. The OG can be generated from highest to lowest volume in the following order: O₂, H₂O, NH₃, CO₂, Xe, and Kr.

FIG. 2 further depicts solids (####, (s)) which can remain in the solid phase upon dissolution of a portion of material 16 and/or form upon dissolution, as a precipitate, for example. These solids can include BaCO₃, SrCO₃, Ln₂(CO₃)₃, Zr (a non-stoichiometric hydrous oxide), a metallic phase of Mo, Tc, Ru, Rh, and Pd, hydrous RuO₂, AgI, In(OH)₃, SbO(OH)₃, hydrous SnO₂, and the transuranic elements. The solids can include Se and As as a non-stoichiometric zirconium selenite and arsenate. Further, the solids can include Pu, Np peroxy carbonates, and/or Am and Cm carbonates.

An example dissolution stoichiometry for UO₂ can be as follows:

UO₂+H₂O₂+3(NH₄)₂CO₃→(NH₄)₄UO₂(CO₃)₃+2NH₄OH  (1)

Consumption of H₂O₂ can be greater than indicated by equation (1). Formation and decomposition of various uranyl peroxide-carbonate complexes can influence H₂O₂ consumption. Fission products and higher actinides may consume a somewhat smaller amount of peroxide, carbonate, and hydroxide. The dissolution can generate hydroxide, but the solution may be buffered and the pH should not change materially.

In accordance with an example dissolution of 15 grams of UO₂:

15 g of UO₂=13.2 g of U=0.0556 mole U Carbonate consumed=0.167 mole Peroxide consumed can be approximately 0.2 mole or greater.

According to example implementations, the method may utilize 150 mL 1.5M (NH₄)₂CO₃ and 30 mL 30% (10.5M) H₂O₂ solution. The final concentrations can be 0.6 M (NH₄)₂CO₃ and 0.6 M H₂O₂. Hydrogen peroxide can be continually decomposing throughout the dissolution and may be below detection limits in a matter of hours. As hydrogen peroxide is consumed, more can be added to continue the oxidation of the UO₂ within the irradiated nuclear fuel.

The volume of O₂ generated can be calculated from the difference between the total volume of H₂O₂ added and the amount consumed by actual oxidation of UO₂ to UO₂ ²⁺. (The amount consumed by oxidation of other actinides and the fission products can be small compared to oxidation of uranium, and may be ignored).

2H₂O₂→2H₂O+O₂  (2)

In accordance with Eq. (2), the total moles H₂O₂ added=0.315 moles, moles H₂O₂ consumed by UO₂=0.0556 moles, and moles H₂O₂ left to decompose to O₂=0.26 moles. The moles O₂ generated=0.13 moles and volume of O₂ gas generated=2.9 liters at room temperature.

If more H₂O₂ is added during the dissolution to make up for decomposition, then the volume of oxygen gas can be greater by that amount. Spent fuel may decompose H₂O₂ faster than unirradiated UO₂.

Upon exposure of material 16 to the solution containing carbonate and peroxide, for example, a mixture that includes at least two of a liquid phase, a solid phase, and a gas phase, are demonstrated to be formed. The phases of the mixture may be separated by classic liquid/solid/gas separation techniques such as filtration and/or evaporation. This separation can include continuous liquid dissolution and separation as well as decanting or batch filtration, for example. Referring again to FIG. 1, filter material 20 may be configured to provide such filtration. Upon filtration, the liquid phase can include a substantial amount of uranium and/or plutonium of the irradiated fuel.

In contrast with the PUREX process for example, embodiments of the present disclosure provide methods, compositions, and/or systems that can be utilized to process irradiated fuel with substantially less adverse environmental impact, hazardous risk, and cost. As demonstrated, embodiments of the present disclosure utilize relatively benign aqueous solutions to process the irradiated fuel and these aqueous solutions can be utilized at ambient temperatures and pressures requiring substantially lower energy costs. The PUREX process, on the other hand, utilizes heated nitric acid solutions which require both substantial environmental and toxic exposure preventive measures as well as substantial energy. Further, and in accordance with example implementations, the solutions utilized to dissolve the irradiated fuel can be considered “green reagents” in that they are generally recyclable or they decompose in water or air without adding waste volume.

Referring to FIG. 3, an overall flow scheme for treating material 16 is shown that includes exposing material 16 to solution 12 to form a mixture and then separating the solid and liquid phases at step 32. Upon separation there remains a liquid fraction 34 as well as a solid fraction 36. The solid fraction can be dissolved yet again in a carbonate solution 38. The carbonate solution can be the ammonium carbonate peroxide solution described herein, as well as other carbonate peroxide solutions, for example.

Upon suspension of the solid 36 into solution 38, a solid phase 44 can be separated at 40. The liquid phase 42 can be combined with liquid phase 34 at 46. According to example implementations this combined liquid phase can be heated at 48 to evaporate off ammonium carbonate in the solution in the form of gas 52 as well as separation at 50 to provide product solution 56 and solid 54. Solid 54 can be combined with the solids 44 to provide solid product material 58. According to example implementations, these processes can be performed while maintaining the temperature of the mixtures below about 100° C.

Utilizing the methods, compositions, and/or systems of the present disclosure to treat the irradiated material, actinides such as neptunium and plutonium may be dissolved with the uranium of the material. Hydrogen peroxide can be maintained in the mixture to retain some actinides in the liquid phase. Actinides in heptavalent forms can be produced in the mixture. These actinides can be a stable portion of the liquid phase, and may be separated from one another by adjusting the pH of the liquid phase. For example, heptavalent neptunium may be stable in aerated solutions at low pH, while at this low pH heptavalent plutonium may precipitate. Alternatively, at high pH, the heptavalent plutonium may be stable in the liquid phase and the heptavalent neptunium may precipitate. The solubility stability of other actinides such as Am and Cm may be exploited to foster separation as well.

With reference to FIGS. 4A and 4B, a more detailed scheme is shown that includes the processing of irradiated nuclear fuel including UO₂ and fission products that also includes the actinides Np, Pu, Am, and Cm, and Sr. This fuel can be exposed to a solution including ammonium carbonate and peroxide. Upon exposure, a heterogeneous mixture including the liquid phase (soluble fraction) and a solid phase (insoluble fraction) are formed. The phases can be separated by filtration to provide separate solid and liquid phases. The soluble species can include those listed as well as mechanically entrained species that may also be present in the liquid phase.

Referring to FIGS. 4A & 4B, the insoluble fraction may include mechanically entrained soluble species. The insoluble fraction can contain Sr, Ba, Zr, Se, As, Mo, Tc, Ru, Rh, Pd (metallic phase), Ag, In, Ge, Sn, Sb, Np, Pu, Am, and Cm. This solid phase may be exposed (resuspended) in an ammonium carbonate solution such as a 1.5M (NH₄)₂CO₃ solution for about 30 min to form another heterogeneous mixture that includes both solid and liquid phases. These phases can be separated and the liquid phases combined. The remaining solid phase may be exposed (washed) to another 1.5M (NH₄)₂CO₃ solution before being combined with solids recovered from further liquid phase processing.

Referring to FIG. 4B, the liquid phase recovered from the initial separation can be about a 0.6M (NH₄)₂CO₃ aqueous solution having U, Rb, Cs, Mo, Tc, Pd, Cd, Ag, As, Se, Te, Br, and/or I. This solution may contain low concentrations of carbonate complexes of Zr, Ln, Np, Pu, Am, and/or Cm. The solution can be warmed to 40-90° C. for 20-40 min. to decompose most of the (NH₄)₂CO₃ and peroxide. This warming can result in the precipitation of a solid phase which can be separated and combined with the previously separated solids. The remaining liquid phase can be about 0.05M (NH₄)₂CO₃ and contain U, Rb, Cs, Mo, Pd, Cd, Ag, As, Se, Te, Br, and/or I.

In accordance with example implementations, the actinides are relegated to the solid phase product while the liquid phase product contains substantially all of the uranium. Thus, the actinides can be separated from the uranium of the irradiated fuel utilizing relatively benign reagents and process parameters. Implementations of the embodiments of the disclosure can provide for the separation of these components while generating little environmental waste and utilizing relatively low amounts of energy.

To compare implementations of the methods, systems, and/or compositions of the present disclosure to that of the prior processing techniques, the following non-limiting examples are provided.

Example 1 Carbonate-Peroxide Dissolution Compared to Nitric Acid Dissolution

Carbonate-Peroxide Dissolution. 50-mg subsamples of fuel can be placed into a 125-mL glass Erlenmeyer flask, 20 mL of saturated ammonium carbonate solution can be added and 10 mL of 30% hydrogen peroxide can be added. (Reagent grade chemicals can be utilized.) A magnetic stir bar can be utilized to mechanically agitate the composition and a watch glass placed over the flask. The mixture can be stirred for one hour, then allowed to stand overnight at ambient temperature. Portions of the fuel can dissolve and demonstrate a bright yellow-orange solution, which can fade over the next few days into something that may appear faintly blue through the yellow hot cell window in which the dissolution can be performed. The solution can be gently taken dry on low heat to evaporate off the ammonium carbonate and any remaining hydrogen peroxide. The dry residue can be dissolved in 5 mL of 12M nitric acid and diluted to 50 mL with 2M nitric acid. The product solution can appear a little dark, with a blue cast, through the yellow hot cell window. The final solution from the carbonate fuel dissolution can be acidic. Elements that form insoluble carbonates, such as strontium and the rare earths, can be ultimately dissolved in the final product solution.

Nitric acid fuel dissolution: 50-mg subsamples of fuel can be placed in 125-mL Erlenmeyer flasks and then 15 mL of 12M nitric acid added. A magnetic stir bar can be utilized to mechanically agitate the composition and a glass funnel can be placed in the top of the Erlenmeyer to contain spray and allow the nitric acid to reflux. The composition can then be warmed to nearly boiling for an hour, or until the fuel has substantially dissolved. The composition may not be taken to dry, so that technetium may not be lost to evaporation (as Tc₂O₇).

After the bulk of the fuel has substantially dissolved, the composition can be centrifuged to separate the undissolved residue. The supernatant liquid can be poured into a volumetric flask, and the residue in the bottom of the centrifuge tube (presumably the Mo, Tc, Ru, Rh, Pd phase) can be returned to the Erlenmeyer flask and heated again for three hours with 10 mL of concentrated nitric acid, with the funnel in place to contain spatter and reflux the nitric acid.

After three hours of heating, a suspension of black particles can be added to the volumetric flask with the previous solution, and then diluted up to 100.0 mL with 2M nitric acid. Any undissolved particles can ultimately be transferred to the volumetric flask with the sample solution.

Results. The nitric acid fuel dissolution and the carbonate-peroxide fuel dissolution can reveal similar results for every analyte except for technetium (see Table 1). The uncertainty given is total propagated uncertainty at 1 standard deviation. The analytical results are statistically the same for both fuel dissolutions, within two standard deviations, for all analytes except technetium.

Results are given in microcuries of analyte per gram of fuel. The two fuel samples are 25 μm and 5 μm sieved samples. “Carb” refers to room temperature ammonium carbonate, hydrogen peroxide fuel dissolution, and “Nitric” means hot 12M nitric acid dissolution.

The fuel can break up and dissolve completely in the carbonate solution, dissolving the UO₂ fuel matrix and a number of other elements, while leaving some other elements in an acid-soluble form. The cesium, europium, americium, strontium, and plutonium can be completely in solution at the end of the carbonate fuel dissolution (in 2M nitric acid).

TABLE 1 Analytical Data, μCi per gram of fuel ± 1 s uncertainty Fuel Sample Cs-134 Cs-137 Eu-154 Eu-155 Am-241 25 μm Carb 9.87E+1 ± 4% 8.61E+4 ± 3% 1.26E+3 ± 2% 2.04E+2 ± 9% 3.08E+3 ± 4% 25 μm Nitric 9.36E+1 ± 4% 8.20E+4 ± 3% 1.23E+3 ± 2% 2.08E+2 ± 8% 2.97E+3 ± 4%  5 μm Carb 9.72E+1 ± 4% 8.44E+4 ± 3% 1.17E+3 ± 2% 2.12E+2 ± 9% 2.85E+3 ± 4%  5 μm Nitric 9.74E+1 ± 4% 8.44E+4 ± 3% 1.15E+3 ± 2% 2.18E+2 ± 15% 2.74E+3 ± 4% Fuel Sample Pu-239 + 240 Pu-238 Sr-90 Tc-99 25 μm Carb 8.61E+2 ± 4% 4.14E+3 ± 3% 4.69E+4 ± 3% 4.88E+0 ± 3% 25 μm Nitric 8.38E+2 ± 2% 4.31E+3 ± 2% 4.59E+4 ± 3% 1.17E+1 ± 3%  5 μm Carb 8.13E+2 ± 4% 4.05E+3 ± 3% 4.53E+4 ± 3% 4.62E+0 ± 3%  5 μm Nitric 8.41E+2 ± 3% 4.26E+3 ± 2% 4.59E+4 ± 3% 1.45E+1 ± 3%

The solid and liquid phases produced utilizing embodiments of the methods, systems, and compositions described may be further processed to separate components within each from the respective liquid and/or solid phases. For example and with reference to FIG. 5, a method for acquiring molybdenum from a uranium comprising material is shown. According to example implementations, material 16 can be exposed to an aqueous solution to form a mixture comprising a solid phase and a liquid phase. With reference to the previous description, material 16 can be freshly irradiated fuel and the solid phase can contain Sr, Ba, Zr, Se, As, Ru, Rh, Pd, Ag, In, Ge, Sn, Sb, Np, and Pu. The liquid phase can contain U, Rb, Cs, Mo, Pd, Cd, Ag, As, Se, Te, Br, Sr, Pu, and/or I. As described the solid and liquid phases can be separated to form two distinct phases, liquid phase 34 and solid phase 36

The liquid phase can be exposed to an adsorbent to remove at least some of the solute from the liquid phase and form an effluent containing the molybdenum. Upon separation, liquid phase 34 can be exposed to an adsorbent such as ion exchange adsorbent 62 and then the effluent from this ion exchange adsorbent processing step can be further purified via liquid/liquid extraction at step 64 to provide material 66 which includes molybdenum. The solids 36 can include fission products.

The methods, systems, and compositions of the present disclosure can thus provide both an environmentally and economically improved process for acquiring particularly valuable metals such as Mo from irradiated fuel. By acquiring these valuable compounds, the processing itself can be made economically feasible and by separating even more mass from portions of the irradiated fuel, the amount of fuel left to be regulated decreases, which decreases cost of environmental handling.

According to example implementations, irradiated nuclear fuel containing fission products can be dissolved in an ammonium carbonate solution. The nuclear fuel may be received in regulated containers and these containers can be first perforated to allow for gas removal. As an example, radiolysis gases can be removed from containers in hotcell by drilling a hole(s) into the containers and evacuating the gases to a cryogenically cooled gas absorbent trap such as a liquid nitrogen-cooled charcoal trap, for example. These traps can be removed and stored to allow for decay of short-lived isotopes of Xe, Kr, I₂, and/or Br₂.

The containers can then be opened to allow for immersion of targets within containers in about 10 L/ea. of 1M ammonium carbonate solution. Each target can contain as much as 500 g of uranium. H₂O₂ can then be added to each mixture to bring the concentration of the mixture to 0.2M H₂O₂ and the mixture gently stirred. Each of these mixtures being considered a dissolver solution.

Referring to FIGS. 6A and 6B, a more detailed scheme for acquiring molybdenum from the dissolver solutions is depicted. As depicted in FIG. 6A, the dissolver solutions can be combined, a hydroxide such as Ba(OH)₂ added, and the solution warmed to decompose any remaining peroxide while maintaining a high carbonate concentration. These liquid phase portions can be acquired via the dissolution of irradiated fuel as described above and/or in accordance with the methods, systems, and compositions of the present disclosure.

This solution can then be filtered to provide both a soluble fraction and an insoluble fraction. The insoluble fraction can include Sr, Ba, Pu, Np, Am, Cm, Zr, Ag, Pd, Rh, Ru, In, Ge, Sn, and/or Sb, for example. This insoluble portion can be exposed to a carbonate solution to provide another liquid phase that may be combined with the soluble fraction. The combined soluble fraction can contain U, Rb, Cs, Mo, Tc, Pd, Cd, Ag, As, Se, Te, Br, and/or I, for example.

The soluble fraction may then be treated in accordance with alternative schemes, neither of which is mutually exclusive. In accordance with one scheme, the soluble fraction can then be passed through a carbonate loaded anion exchange resin capturing substantially all of the U but allowing effluent containing substantially all remaining components of the liquid fraction to pass, the Mo-effluent. This resin can be 8 L, 15 L, and/or from 8 L to 15 L. This effluent can contain Rb, Cs, Pd, Cd, Ag, Mo, Tc, As, Se, Te, Br, and/or I. In accordance with this scheme, the resin will be sufficiently robust to radiolysis from high dose cationic species in the soluble fraction for batches as large as 20 targets, for example.

In accordance with an alternative scheme, the soluble fraction shown in FIG. 6A and obtained from the filtered dissolver solution can then be passed through a cation exchange resin, such as a NH₄ ⁺-form cation exchange resin, and rinsed with an ammonium carbonate solution such as a 0.005M (NH₄)₂CO₃ solution to provide an effluent that contains UO₂(CO₃)₃ ⁴⁻, MoO₄ ²⁻, TcO₄ ⁻, AsO₄ ³⁻, SeO₃ ²⁻, TeO₃ ²⁻Br⁻ and/or I⁻, the alternative Mo-effluent. Either one or both of these Mo-effluents can be further treated by organic extraction as described below.

The Mo-effluent recovered from the anion resin may also be further treated with a cation resin prior to organic extraction. The Mo-effluent can then be passed through an ammonium loaded ion exchange resin to capture Rb, Cs, Pd, Cd, and/or Ag. The effluent passing this ammonium loaded resin can include Mo, Tc, As, Se, Te, Br, and/or I. The captured components can be washed from the resin and combined as waste if desired.

The effluents from resins can subjected to liquid/liquid extraction to acquire the Mo from the mixture of Mo, Tc, As, Se, Te, Br, and/or I. This effluent can primarily be an aqueous carbonate solution and this solution can be exposed to a primarily organic solution such as 8-hydroxyquinoline in chloroform, for example. The Mo can be removed from the solution and the remaining aqueous phase discarded if desired. In accordance with example implementations, the systems, methods, and compositions of the present disclosure can provide for the dissolution of the irradiated fuel with solutions that are manageable when utilizing ion exchange purification techniques. For example, the ammonium carbonate system of the solutions can allow for a substantially efficient purification utilizing ion exchange resin under aqueous conditions, while only a single step of the method utilizes an organic solvent, thereby providing methods that can recover Mo under environmentally as well as economically friendly conditions.

In compliance with the statute, embodiments of the invention have been described in language more or less specific as to structural and methodical features. It is to be understood, however, that the entire invention is not limited to the specific features and/or embodiments shown and/or described, since the disclosed embodiments comprise forms of putting the invention into effect. The invention is, therefore, claimed in any of its forms or modifications within the proper scope of the appended claims appropriately interpreted in accordance with the doctrine of equivalents. 

1. A composition comprising irradiated nuclear fuel and ammonium.
 2. The composition of claim 1 wherein at least a portion of the composition is liquid phase and at least another portion of the composition is solid phase.
 3. The composition of claim 2 wherein at least some of the ammonium is comprised by the liquid phase.
 4. The composition of claim 2 wherein the nuclear fuel comprises fission products, and at least some of the fission products is comprised by the solid phase.
 5. The composition of claim 2 wherein the nuclear fuel comprises uranium, and at least some of the uranium is comprised by the liquid phase.
 6. The composition of claim 1 wherein the fuel is comprised by particles having an average size of less than 200 μm.
 7. A composition comprising: irradiated nuclear fuel; carbonate; and peroxide.
 8. The composition of claim 7 wherein the peroxide is hydrogen peroxide.
 9. The composition of claim 7 wherein the irradiated nuclear fuel comprises both fission products and uranium.
 10. The composition of claim 8 wherein at least a portion of the composition is liquid phase and at least another portion of the composition is solid phase, the solid phase comprising at least a portion of the fission products, and the liquid phase comprising at least a portion of the uranium.
 11. The composition of claim 7 further comprising UO₂(CO₃)₃ ⁴⁻.
 12. The composition of claim 11 further comprising a liquid phase comprising water and the UO₂(CO₃)₃ ⁴⁻.
 13. The composition of claim 7 wherein the fuel is comprised by particles having an average size of from about 5 μm to about 200 μm.
 14. The composition of claim 13 wherein the average size is from about 25 μm to about 200 μm.
 15. The composition of claim 13 wherein the average size is from about 5 μm to about 25 μm.
 16. A method for treating irradiated nuclear fuel, the method comprising exposing the fuel to a carbonate-peroxide solution to dissolve at least a portion of the uranium into the solution.
 17. The method of claim 16 wherein the carbonate-peroxide solution comprises ammonium carbonate and peroxide.
 18. The method of claim 17 wherein the ammonium carbonate is at least 0.1 M of the solution prior to being exposed to the fuel.
 19. The method of claim 17 wherein the peroxide is at least 0.05 M of the solution prior to being exposed to the fuel.
 20. The method of claim 17 wherein the concentration of ammonium carbonate within the solution is greater than the concentration of peroxide within the solution.
 21. A method for treating irradiated nuclear fuel, the method comprising: exposing the fuel to an ammonium solution to dissolve at least a portion of the uranium into the solution; and removing at least some of the ammonium from the solution to acquire the uranium.
 22. The method of claim 21 wherein the ammonium solution comprises ammonium carbonate and the removing comprises heating the solution to evaporate at least some of the ammonium carbonate from the solution and form a product solution comprising at least some of the uranium.
 23. The method of claim 22 wherein the product solution comprises both a solid phase and a liquid phase, the solid phase comprising fission products and the liquid phase comprising the uranium.
 24. The method of claim 23 further comprising separating the solid phase from the liquid phase to acquire the uranium in the liquid phase.
 25. The method of claim 24 further comprising exposing the liquid phase to an ion exchange resin.
 26. The method of claim 24 further comprising exposing the liquid phase to an extraction solution.
 27. A method for treating irradiated nuclear fuel, the method comprising: preparing a mixture comprising the fuel and an aqueous solution; and maintaining the mixture below a temperature of 100° C. while dissolving at least a portion of the uranium of the fuel into the solution.
 28. The method of claim 27 wherein the aqueous solution comprises one or more of carbonate, ammonium, and peroxide.
 29. The method of claim 27 further comprising separating the uranium from the solution.
 30. The method of claim 29 wherein the separating comprises an ion exchange and/or liquid/liquid extraction.
 31. The method of claim 27 further comprising agitating the mixture while maintaining the mixture below a temperature of 100° C.
 32. A method for acquiring molybdenum from a uranium comprising material, the method comprising: exposing the material to an aqueous solution to form a mixture comprising a solid phase and a liquid phase; separating the solid phase from the liquid phase; and exposing at least a portion of the liquid phase to an adsorbent to remove at least some of the solute from the liquid phase and form an effluent containing the molybdenum.
 33. The method of claim 32 wherein the material is irradiated nuclear fuel.
 34. The method of claim 32 wherein the aqueous solution comprises one or more of ammonium, carbonate, and peroxide.
 35. The method of claim 32 wherein the solid phase comprises fission products.
 36. The method of claim 32 wherein the adsorbent comprises an ion exchange resin.
 37. The method of claim 32 further comprising exposing the effluent to an extraction solution to purify the molybdenum. 